Inventor · disambiguated record
Peter Sturdza
Also filed as: STURDZA PETER
18 granted patents·43 citations·filing 2007–2020
91Inventor score
Files withAERION CORP6AERION INTELLECTUAL PROPERTY MAN CORPORATION6RAJNARAYAN DEV2RODRIGUEZ DAVID L2STURDZA PETER1
Top patents by PatentIndex Score
18 records- 0188US8457939B2Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow meshRODRIGUEZ DAVID L·Filed 2010·Granted Jun 4, 2013·14 cites·20 claims
- 0280US10296672B2Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow meshAERION CORP·Filed 2014·Granted May 21, 2019·5 cites·20 claims
- 0378US8437990B2Generating a simulated fluid flow over an aircraft surface using anisotropic diffusionRODRIGUEZ DAVID L·Filed 2011·Granted May 7, 2013·6 cites·20 claims
- 0477US8935140B2Generating inviscid and viscous fluid-flow simulations over a surface using a fluid-flow meshAERION CORP·Filed 2013·Granted Jan 13, 2015·4 cites·20 claims
- 0575US8538738B2Predicting transition from laminar to turbulent flow over a surfaceRAJNARAYAN DEV·Filed 2011·Granted Sep 17, 2013·5 cites·32 claims
- 0667US9348956B2Generating a simulated fluid flow over a surface using anisotropic diffusionAERION CORP·Filed 2013·Granted May 24, 2016·2 cites·20 claims
- 0763US8892408B2Generating inviscid and viscous fluid flow simulations over a surface using a quasi-simultaneous techniqueSTURDZA PETER·Filed 2011·Granted Nov 18, 2014·3 cites·24 claims
- 0853US7946535B2Highly efficient supersonic laminar flow wingAERION CORP·Filed 2007·Granted May 24, 2011·4 cites·15 claims
- 0951US9494482B2Predicting transition from laminar to turbulent flow over a surface using mode-shape parametersAERION CORP·Filed 2013·Granted Nov 15, 2016·0 cites·36 claims
- 1050US10634581B2Predicting transition from laminar to turbulent flow over a surface using mode-shape parametersRAJNARAYAN DEV·Filed 2016·Granted Apr 28, 2020·0 cites·20 claims
- 1144US9418202B2Predicting transition from laminar to turbulent flow over a surfaceAERION CORP·Filed 2013·Granted Aug 16, 2016·0 cites·25 claims
- 1239US8272594B2Laminar flow wing optimized for supersonic cruise aircraftTRACY RICHARD R·Filed 2009·Granted Sep 25, 2012·0 cites·37 claims
- 1338USD950467SAirplaneAERION INTELLECTUAL PROPERTY MAN CORPORATION·Filed 2020·Granted May 3, 2022·0 cites·1 claims
- 1438USD950468SAirplaneAERION INTELLECTUAL PROPERTY MAN CORPORATION·Filed 2020·Granted May 3, 2022·0 cites·1 claims
- 1538USD950465SAirplaneAERION INTELLECTUAL PROPERTY MAN CORPORATION·Filed 2020·Granted May 3, 2022·0 cites·1 claims
- 1638USD950466SAirplaneAERION INTELLECTUAL PROPERTY MAN CORPORATION·Filed 2020·Granted May 3, 2022·0 cites·1 claims
- 1738USD950469SAirplaneAERION INTELLECTUAL PROPERTY MAN CORPORATION·Filed 2020·Granted May 3, 2022·0 cites·1 claims
- 1838USD950470SAirplaneAERION INTELLECTUAL PROPERTY MAN CORPORATION·Filed 2020·Granted May 3, 2022·0 cites·1 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →